ES2359518T3 - Procedimiento y aparato para indicar el estado de funcionamiento de un motor de aviación. - Google Patents

Procedimiento y aparato para indicar el estado de funcionamiento de un motor de aviación. Download PDF

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Publication number
ES2359518T3
ES2359518T3 ES07076060T ES07076060T ES2359518T3 ES 2359518 T3 ES2359518 T3 ES 2359518T3 ES 07076060 T ES07076060 T ES 07076060T ES 07076060 T ES07076060 T ES 07076060T ES 2359518 T3 ES2359518 T3 ES 2359518T3
Authority
ES
Spain
Prior art keywords
engine
speed
indicating
recited
indicator
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
ES07076060T
Other languages
English (en)
Spanish (es)
Inventor
Samuel T. Clark
Andrew W. Houck
Joseph A. Sikora
Roglenda R. Bowe
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=39273808&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ES2359518(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ES2359518T3 publication Critical patent/ES2359518T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Instrument Panels (AREA)
ES07076060T 2006-12-07 2007-12-07 Procedimiento y aparato para indicar el estado de funcionamiento de un motor de aviación. Active ES2359518T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US635418 2006-12-07
US11/635,418 US7679529B2 (en) 2006-12-07 2006-12-07 Method and apparatus for indicating operational state of aircraft engine

Publications (1)

Publication Number Publication Date
ES2359518T3 true ES2359518T3 (es) 2011-05-24

Family

ID=39273808

Family Applications (1)

Application Number Title Priority Date Filing Date
ES07076060T Active ES2359518T3 (es) 2006-12-07 2007-12-07 Procedimiento y aparato para indicar el estado de funcionamiento de un motor de aviación.

Country Status (5)

Country Link
US (1) US7679529B2 (de)
EP (1) EP1930239B1 (de)
AT (1) ATE495101T1 (de)
DE (1) DE602007011877D1 (de)
ES (1) ES2359518T3 (de)

Families Citing this family (11)

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US20110029804A1 (en) * 2008-12-22 2011-02-03 Honeywell International Inc. Fleet mission management system and method using health capability determination
US20100162027A1 (en) * 2008-12-22 2010-06-24 Honeywell International Inc. Health capability determination system and method
US8779945B2 (en) 2010-03-17 2014-07-15 Sikorsky Aircraft Corporation Virtual ice accretion meter display
US9046891B2 (en) 2010-10-22 2015-06-02 Honeywell International Inc. Control effector health capabilities determination reasoning system and method
EP3124385B1 (de) * 2010-12-22 2017-10-25 Bell Helicopter Textron Inc. Stromsicherheitssystem
WO2016145325A1 (en) * 2015-03-12 2016-09-15 Sikorsky Aircraft Corporation Conditional engine igniters
CN108137160B (zh) * 2015-09-30 2021-10-01 庞巴迪公司 用于呈现飞机发动机的操作状态的方法和系统
US9950805B2 (en) * 2015-10-26 2018-04-24 The Boeing Company Aircraft engine fan speed display improvements for enhanced monitoring and thrust setting ability
US11225915B2 (en) 2017-11-16 2022-01-18 General Electric Company Engine core speed reducing method and system
EP3534246B1 (de) * 2018-02-27 2023-05-24 Gulfstream Aerospace Corporation Trendanzeigen für avioniksysteme
CN110411439B (zh) * 2019-07-15 2021-07-09 北京控制工程研究所 一种根据星能量等级生成仿真星点的方法、装置及介质

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3512128A (en) * 1967-04-26 1970-05-12 Firestone Tire & Rubber Co Engine control warning system
US4044709A (en) * 1975-09-29 1977-08-30 Pacer Systems, Inc. Omnidirectional speed cockpit display
US4060979A (en) * 1975-11-19 1977-12-06 United Technologies Corporation Stall warning detector for gas turbine engine
US4325123A (en) * 1978-07-28 1982-04-13 The Boeing Company Economy performance data avionic system
DE3315386A1 (de) 1983-04-28 1984-10-31 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Anzeigegeraet zur bildlichen darstellung von messwerten
US4750127A (en) * 1985-10-31 1988-06-07 The Boeing Company Energy compensated target speed for aircraft descent
US5353022A (en) * 1987-08-06 1994-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5050081A (en) 1988-11-14 1991-09-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and system for monitoring and displaying engine performance parameters
US5404766A (en) 1992-10-01 1995-04-11 Honeywell Inc. Rotating round dial aircraft engine instruments
US5422625A (en) * 1993-04-16 1995-06-06 Moriyama Kogyo Kabushiki Kaisha Control system for engine speed meter
US5668542A (en) 1995-07-03 1997-09-16 The United States Of America As Represented By The Secretary Of The Air Force Color cockpit display for aircraft systems
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
US6085129A (en) * 1997-11-14 2000-07-04 Rockwell Collins, Inc. Integrated vertical profile display
US6118385A (en) 1998-09-09 2000-09-12 Honeywell Inc. Methods and apparatus for an improved control parameter value indicator
US6188937B1 (en) * 1998-09-30 2001-02-13 Honeywell International Inc. Methods and apparatus for annunciation of vehicle operational modes
US6505594B1 (en) * 1999-08-23 2003-01-14 Toyota Jidosha Kabushiki Kaisha Control apparatus for internal combustion engine and method of controlling internal combustion engine
US6735505B2 (en) * 2002-01-17 2004-05-11 Cubic Defense Systems, Inc. Aircraft flight and voice data recorder system and method
US7088264B2 (en) * 2002-03-14 2006-08-08 Honeywell International Inc. Flight safety system monitoring combinations of state values
US7142131B2 (en) 2002-07-03 2006-11-28 The Boeing Company Method and apparatus for displaying aircraft engine characteristics
EP1378446B1 (de) 2002-07-03 2017-08-09 The Boeing Company Verfahren und Vorrichtung zum Anzeigen Flugzeugmotorparametern
JP4087686B2 (ja) * 2002-11-21 2008-05-21 ヤマハマリン株式会社 船外機用エンジンの回転変動制御システム
US7053796B1 (en) 2003-02-27 2006-05-30 Rockwell Collins, Inc. Multi-dimensional instruments for monitoring engine and system parameters
FR2871437B1 (fr) * 2004-06-15 2006-08-18 Eurocopter France Indicateur de pilotage permettant de predire l'evolution du regime de rotation du rotor principal d'un giravion
FR2871520B1 (fr) * 2004-06-15 2008-12-26 Eurocopter France Indicateur de pilotage permettant de predire l'evolution des parametres de surveillance d'un turbomoteur
US7414544B2 (en) * 2005-01-28 2008-08-19 Bell Helicopter Textron, Inc. Power situation indicator

Also Published As

Publication number Publication date
ATE495101T1 (de) 2011-01-15
DE602007011877D1 (de) 2011-02-24
EP1930239A1 (de) 2008-06-11
US20080136677A1 (en) 2008-06-12
EP1930239B1 (de) 2011-01-12
US7679529B2 (en) 2010-03-16

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